US8118075B2 - System and method for disassembling laminated substrates - Google Patents

System and method for disassembling laminated substrates Download PDF

Info

Publication number
US8118075B2
US8118075B2 US12/009,372 US937208A US8118075B2 US 8118075 B2 US8118075 B2 US 8118075B2 US 937208 A US937208 A US 937208A US 8118075 B2 US8118075 B2 US 8118075B2
Authority
US
United States
Prior art keywords
assembly
cutting member
elongated
amount
planar
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active, expires
Application number
US12/009,372
Other versions
US20090183615A1 (en
Inventor
James D. Sampica
Paul R. Nemeth
Tracy J. Barnidge
Vincent P. Marzen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rockwell Collins Inc
Original Assignee
Rockwell Collins Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
US case filed in Delaware District Court litigation Critical https://portal.unifiedpatents.com/litigation/Delaware%20District%20Court/case/1%3A20-cv-01510 Source: District Court Jurisdiction: Delaware District Court "Unified Patents Litigation Data" by Unified Patents is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Rockwell Collins Inc filed Critical Rockwell Collins Inc
Priority to US12/009,372 priority Critical patent/US8118075B2/en
Priority to US12/009,482 priority patent/US8936057B2/en
Assigned to ROCKWELL COLLINS, INC. reassignment ROCKWELL COLLINS, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BARNIDGE, TRACY J., MARZEN, VINCENT P., NEMETH, PAUL R., SAMPICA, JAMES D.
Priority to CN201510005057.5A priority patent/CN104765168B/en
Priority to KR1020107017278A priority patent/KR101625880B1/en
Priority to EP16188276.6A priority patent/EP3135490B1/en
Priority to PCT/US2009/031151 priority patent/WO2009091923A2/en
Priority to KR1020167013740A priority patent/KR101763710B1/en
Priority to EP14161363.8A priority patent/EP2749412B1/en
Priority to CN200980107294.5A priority patent/CN101971080B/en
Priority to JP2010543255A priority patent/JP5431364B2/en
Priority to EP09702309.7A priority patent/EP2243054A4/en
Publication of US20090183615A1 publication Critical patent/US20090183615A1/en
Publication of US8118075B2 publication Critical patent/US8118075B2/en
Application granted granted Critical
Priority to JP2013251126A priority patent/JP5762516B2/en
Priority to US14/270,563 priority patent/US9638944B1/en
Priority to JP2015116688A priority patent/JP5869171B2/en
Priority to JP2015116716A priority patent/JP5869172B2/en
Priority to JP2016001165A priority patent/JP6186452B2/en
Active legal-status Critical Current
Adjusted expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D1/00Cutting through work characterised by the nature or movement of the cutting member or particular materials not otherwise provided for; Apparatus or machines therefor; Cutting members therefor
    • B26D1/01Cutting through work characterised by the nature or movement of the cutting member or particular materials not otherwise provided for; Apparatus or machines therefor; Cutting members therefor involving a cutting member which does not travel with the work
    • B26D1/547Cutting through work characterised by the nature or movement of the cutting member or particular materials not otherwise provided for; Apparatus or machines therefor; Cutting members therefor involving a cutting member which does not travel with the work having a wire-like cutting member
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D3/00Cutting work characterised by the nature of the cut made; Apparatus therefor
    • B26D3/28Splitting layers from work; Mutually separating layers by cutting
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B26HAND CUTTING TOOLS; CUTTING; SEVERING
    • B26DCUTTING; DETAILS COMMON TO MACHINES FOR PERFORATING, PUNCHING, CUTTING-OUT, STAMPING-OUT OR SEVERING
    • B26D7/00Details of apparatus for cutting, cutting-out, stamping-out, punching, perforating, or severing by means other than cutting
    • B26D7/08Means for treating work or cutting member to facilitate cutting
    • B26D7/10Means for treating work or cutting member to facilitate cutting by heating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B17/00Layered products essentially comprising sheet glass, or glass, slag, or like fibres
    • B32B17/06Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material
    • B32B17/10Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin
    • B32B17/10005Layered products essentially comprising sheet glass, or glass, slag, or like fibres comprising glass as the main or only constituent of a layer, next to another layer of a specific material of synthetic resin laminated safety glass or glazing
    • B32B17/10807Making laminated safety glass or glazing; Apparatus therefor
    • B32B17/1099After-treatment of the layered product, e.g. cooling
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B43/00Operations specially adapted for layered products and not otherwise provided for, e.g. repairing; Apparatus therefor
    • B32B43/006Delaminating
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2457/00Electrical equipment
    • B32B2457/20Displays, e.g. liquid crystal displays, plasma displays
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S83/00Cutting
    • Y10S83/907Coiled wire cutting
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/11Methods of delaminating, per se; i.e., separating at bonding face
    • Y10T156/1153Temperature change for delamination [e.g., heating during delaminating, etc.]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/19Delaminating means
    • Y10T156/1911Heating or cooling delaminating means [e.g., melting means, freezing means, etc.]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/19Delaminating means
    • Y10T156/1961Severing delaminating means [e.g., chisel, etc.]
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/19Delaminating means
    • Y10T156/1961Severing delaminating means [e.g., chisel, etc.]
    • Y10T156/1967Cutting delaminating means
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/02Other than completely through work thickness
    • Y10T83/0267Splitting
    • Y10T83/0274By use of endless band or chain knife
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/02Other than completely through work thickness
    • Y10T83/0267Splitting
    • Y10T83/0296With infeeding of work
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/04Processes
    • Y10T83/0405With preparatory or simultaneous ancillary treatment of work
    • Y10T83/041By heating or cooling
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/04Processes
    • Y10T83/0515During movement of work past flying cutter
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/707By endless band or chain knife
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/707By endless band or chain knife
    • Y10T83/7101With tool in-feed
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/727With means to guide moving work
    • Y10T83/73Guide fixed to or integral with stationary tool element
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T83/00Cutting
    • Y10T83/929Tool or tool with support
    • Y10T83/9292Wire tool

Definitions

  • the present application is related to and claims the benefit of earliest available effective filing date(s) from the following listed application(s) (the “Related Applications”) (e.g., claims earliest available priority dates for other than provisional patent applications; claims benefits under 35 USC ⁇ 119(e) for provisional patent applications), and incorporates by reference in its entirety all subject matter of the following listed application(s); the present application also claims the earliest available effective filing date(s) from, and also incorporates by reference in its entirety all subject matter of any and all parent, grandparent, great-grandparent, etc. applications of the Related Application(s) to the extent such subject matter is not inconsistent herewith:
  • the present invention relates generally to laminated substrates. More specifically, the present invention relates to disassembling laminated substrates.
  • Laminated displays are generally constructed for deployment within potentially harsh environments.
  • These harsh environments are high and low ambient temperatures, dust, moisture, vibration, shock and the inevitable risk of abuse by users who are operating under pressure-packed conditions.
  • These challenges can be especially difficult when designing the displays that provide critical user interface functions and also are exposed to a risk of damage.
  • a display may acquire defects during the lamination process or may be damaged by the manufacturer, shipper or user during handling.
  • Apparatus may comprise a substantially planar assembly, the substantially planar assembly comprising a plate assembly suitable for receiving a laminated substrate assembly and a guide assembly configured to guide the plate assembly in at least one direction, a cutting member housing assembly positioned on a first side of the substantially planar assembly suitable for containing an elongated cutting member and releasing an amount of the elongated cutting member and a cutting member receiving assembly positioned on a second side of the substantially planar assembly, substantially opposite from the first side of the planar assembly suitable for receiving an amount of the elongated cutting member.
  • At least one of the cutting member housing assembly or the cutting member receiving assembly is configured to provide an amount of tension to the elongated cutting member as the elongated cutting member is released by the cutting member housing assembly or received by the cutting member receiving assembly and the elongated cutting member is configured to remove an amount of adhesive from an adhesive layer of the laminated substrate assembly positioned on a top surface of the plate assembly of the planar assembly as the amount of the elongated cutting member is transferred from the cutting member housing assembly to the cutting member receiving assembly.
  • Method may comprise providing a planar assembly, placing a laminated substrate assembly on a surface of the planar assembly, determining a position of an adhesive layer of the laminated substrate assembly, providing an elongated cutting member housing assembly configured to house an amount of an elongated cuffing member, providing an elongated cutting member receiving assembly configured to receive an amount of the elongated cutting member, positioning an amount of the elongated cutting substantially between two layers of a laminated substrate assembly along a length of the adhesive layer of the laminated substrate assembly, and transferring an amount of elongated cutting member from the cutting member housing assembly to the cutting member receiving assembly by rotating at least one of the cutting member housing assembly or the cutting member receiving assembly to draw the elongated cutting member along the length of the adhesive layer.
  • the amount of elongated cutting member is configured to remove at least a portion of an adhesive as the amount of elongated cutting member is transferred from the cutting member housing assembly to the cutting member receiving assembly.
  • System may comprise a substantially planar assembly.
  • the substantially planar assembly may comprise a surface for receiving a laminated substrate assembly and a separation assembly.
  • the separation assembly may further comprise an elongated cutting member, a cutting member housing assembly and a cutting member receiving assembly suitable for receiving the elongated cutting member.
  • the cutting member housing assembly may be suitable for containing and releasing the elongated cutting member and the cutting member receiving assembly may be suitable for receiving the elongated cutting member.
  • System may further comprise a control assembly for controlling the separation assembly.
  • FIG. 1 is an isometric view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention
  • FIG. 2 is an additional isometric view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention
  • FIG. 3 is a further additional isometric view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention
  • FIG. 4 is a side view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention.
  • FIG. 5 is a top view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention.
  • FIG. 6 is an isometric illustration of laminated substrates separated via the apparatus for separating laminated substrates according to an exemplary embodiment of the present invention.
  • FIG. 7 is a block diagram of a system for separating laminated substrates according to an exemplary embodiment of the present invention
  • FIG. 8 is a flow diagram of a method for separating laminated substrates according to an exemplary embodiment of the present invention.
  • FIG. 9 is an additional flow diagram of a method for separating laminated substrates according to an exemplary embodiment of the present invention.
  • Apparatus 100 may comprise a substantially planar assembly 102 , the substantially planar assembly 102 comprising a plate assembly 104 suitable for receiving a laminated substrate assembly and a guide assembly 106 configured to guide the plate assembly 104 in at least one direction, a cutting member housing assembly 108 positioned on a first side of the substantially planar assembly 102 suitable for containing an elongated cutting member 110 and releasing an amount of the elongated cutting member 110 and a cutting member receiving assembly 112 positioned on a second side of the substantially planar assembly 102 , substantially opposite from the first side of the planar assembly 102 suitable for receiving an amount of the elongated cutting member 110 .
  • At least one of the cutting member housing assembly 108 or the cutting member receiving assembly 112 is configured to provide an amount of tension to the elongated cutting member 110 as the elongated cutting member 110 is released by the cutting member housing assembly 108 or received by the cutting member receiving assembly 112 and the elongated cutting member 110 is configured to remove an amount of adhesive from an adhesive layer of the laminated substrate assembly positioned on the top surface of the plate assembly 104 of the planar assembly 102 as the amount of the elongated cutting member 110 is transferred from the cutting member housing assembly 108 to the cutting member receiving assembly 112 .
  • a laminated substrate assembly 302 is shown on an apparatus 100 for separating a laminated substrate assembly.
  • a “substrate” as used herein may further refer to any rigid or semi-rigid planar surface of glass, plastic, film, and/or metal coated with an adhesive.
  • a laminated substrate assembly 302 may comprise an anti-reflective/anti-glare substrate, a touch panel, a glass substrate, a polarizing film substrate, an LCD, an electrode plane including a conductive coating (e.g., indium-tin oxide) substrate, another glass substrate, and/or another polarizing film substrate.
  • a conductive coating e.g., indium-tin oxide
  • Laminated substrate assembly 302 may be, for example, a conventional display comprising, for example, at least two substrates between which the liquid crystal material is disposed and a third substrate adhered to a top layer of the conventional display. Lines of electrodes may be patterned onto the first and second substrates. A third substrate may be an optically bonded safety/filter glass or touch screen. Adhesive layer may composed of pressure sensitive adhesive, or any adhesive that forms a bond when pressure is applied to marry the adhesive with the adherend.
  • adhesive layer may be composed of a structural adhesive, i.e., any adhesive that hardens via processes such as evaporation of solvent or water (white glue), reaction with radiation (dental adhesives), chemical reaction (two part epoxy), or cooling, or any combination of structural and pressure sensitive adhesive.
  • the adhesive layer may be composed of have a thickness, for example, from a range of about 20 microns to 3000 microns.
  • Pressure sensitive adhesive may be any adhesive suitable for forming a bond when pressure is applied to engage the adhesive with the adherend.
  • the pressure-sensitive adhesive may be a viscoelastic material utilized in this study, energy dissipation through large-scale bridging effects as well as time-dependent strain-rate effects must be considered.
  • a plate assembly 104 of the planar assembly 102 may be a substantially horizontal surface (e.g. table top).
  • additional embodiments may include a planar assembly 102 including a plate assembly 104 that is substantially convexly or concavely curved (e.g. semi-spherical) or arced, may undulate (e.g. sinusoidally), may be configured to receive corner portions formed at any angle and/or may be customized to receive laminated substrate assemblies formed in any shape or abstract formation.
  • Planar assembly 102 may be composed substantially of metal, metal alloy, heat resistive plastic, ceramic, silicone or any other natural or synthetic material capable of forming a substantially smooth, flat surface.
  • Planar assembly plate assembly 104 may comprise at least one guide marker 114 (e.g. a rectangular outline) formed on or imbedded into a top surface of the plate assembly 104 .
  • Guide marker 114 may provide placement or movement guidance for displays of known or predetermined size and shape.
  • Plate assembly top surface may comprise a plurality of guide markers 114 outlining a plurality of laminated substrate display sizes and/or shapes.
  • the plate assembly 104 of the planar assembly 102 may be configured to receive an amount of heat from a heat source.
  • the heat source is a uniform heat source configured to uniformly heat a region of the plate assembly 104 of the planar assembly 102 .
  • the planar assembly 102 may comprise a plurality of heating mechanisms configured provide substantially uniform heating of the plate assembly 104 of the planar assembly 102 .
  • a laminated substrate assembly 302 placed on the plate assembly 104 of the planar assembly 102 may receive heat from the heated plate assembly 104 . Heating of the plate assembly 104 of the planar assembly 102 , and thus, the laminated substrate assembly 302 may be to a temperature not lower than the softening temperature of the adhesive utilized to bond the substrates.
  • Guide assembly 106 may be a rail or post along which the plate assembly 104 may glide or move along. Guide assembly 106 may be manually operated or motorized as desired, and may provide substantially linear movement of the plate assembly 104 of the planar assembly 102 . In additional embodiments, guide assembly 106 may be configured to match the shape or path determined by the shape of the plate assembly 104 .
  • the elongated cutting member 110 may be a wire or any other such cylindrical, flat and/or otherwise shaped, elongated string of drawn material such as metal, metal alloy, plastic, silicone or any other natural or synthetic material comprising an appropriate tensile strength and suitable to be elongated into string or wire form.
  • the metals suitable for forming an elongated cutting member 110 may include platinum, silver, iron, copper, aluminum and gold.
  • the cutting member housing assembly 108 may be a first hub.
  • first hub may be substantially cylindrical.
  • cutting member housing assembly 108 may be a flanged cylinder, reel or other such housing for an amount of an elongated cutting member 110 comprising a flange 118 as shown in FIG. 2 , or an unflanged cylinder, reel or other such housing for an amount of an elongated cutting member 110 and on which the elongated cutting member 110 may be wound.
  • any shape may be utilized to form the first hub.
  • at least a portion of the elongated cutting member 110 may be wrapped substantially about the first hub.
  • Cutting member housing assembly 108 may be motorized or manually operated.
  • Cutting member housing assembly 108 may rotate along an axis to release an amount of the elongated cutting member 110 as necessary to maintain elongated cutting member 110 at a desired tautness.
  • the cutting member receiving assembly 112 may be a second hub configured to receive at least a portion of the elongated cutting member 110 .
  • second hub may be substantially cylindrical.
  • cutting member receiving assembly 112 may be a flanged or unflanged cylinder or reel on which the elongated cutting member 110 may be wound.
  • any shape may be utilized to form the second hub.
  • At least a portion of an elongated cutting member 110 may be configured to wrap substantially about the second hub after at least a portion of the adhesive has been removed from the laminated substrate assembly 302 .
  • Cutting member receiving assembly 112 may be motorized or manually operated.
  • Cutting member receiving assembly 112 may rotate along an axis to receive an amount of the elongated cutting member 110 as necessary to maintain elongated cutting member 110 at a desired tautness.
  • the apparatus 100 may further comprise a calibration assembly 116 configured to calibrate a zero point relative to a top surface of the plate assembly 104 of the planar assembly 102 .
  • a laminated assembly adhesive joint may be at any height relative to a top surface of the plate assembly 104 of the planar assembly 102 when the laminated assembly 302 ( FIG. 3 ) is placed on the top surface of the plate assembly 104 of the planar assembly 102 .
  • a calibration assembly 116 may be configured to mark the top surface 104 of the planar assembly 102 as a zero distance point.
  • Calibration assembly 116 may also receive an input relating to a distance from the top surface of the plate assembly 104 (e.g.
  • the calibration assembly 116 may also be connected to a database of known laminated substrate assembly thicknesses, including a thickness of any individual components of the laminated substrate assembly 302 . Calibration assembly 116 may then determine a set point for the elongated cutting member 110 above the top surface 104 of the planar assembly 102 . Set point may be, for example, at a distance above the zero point, designated by distance 122 in FIG. 1 and FIG.
  • Calibration assembly 116 may be electrically connected to at least one of the cutting member housing assembly 108 and the cutting member receiving assembly 112 , and thus may be comprised of at least two separate calibration components (each designated as 116 ). Each of the calibration assembly 116 components may raise or lower at least a portion of the elongated cutting member 110 .
  • a database of known laminated substrate assembly component thicknesses may be utilized by the calibration assembly 116 to determine a set point for the elongated cutting member 110 at a distance above the zero point corresponding with the thickness of any laminated assembly components located below the adhesive layer of the laminated substrate assembly 302 plus any additional amount as desired by an operator.
  • the apparatus 100 may further comprise an edge assembly (not shown) configured to attach to a top surface of the plate assembly 104 of the planar assembly 102 and guide the laminated substrate in a direction substantially orthogonal to the elongated cutting member 110 .
  • Edge assembly may facilitate the application of uniform force to the laminated substrate assembly 302 . For instance, as a laminated substrate assembly 302 travels along the planar assembly 102 in a direction orthogonal to the motion of the elongated cutting member 110 , the motion may be substantially uniform across the leading edge of the laminated substrate assembly 302 by force applied to a trailing edge of the laminated substrate assembly via the edge assembly.
  • apparatus 100 may be configured to remove a vertically positioned display.
  • a planar assembly may comprise a vertical stability assembly configured to apply an amount of pressure to at least two surfaces of a laminated substrate assembly 302 to provide vertical stability for the laminated substrate assembly 302 .
  • Cutting assembly may be configured to traverse through an adhesive layer while the laminated substrate assembly 302 is vertically positioned and stationary.
  • a cutting member housing assembly and a cutting member receiving assembly may be as described above and in FIGS. 1-5 configured to house and receive an elongated cutting member (e.g. a wire), and may further comprise a transport assembly configured to raise or lower the cutting member housing assembly and the cutting member receiving assembly as necessary to traverse through the laminated substrate along the adhesive layer.
  • transport assembly may be individually or simultaneously controlled.
  • Transport mechanism may be manual, hydraulic, motorized or comprise any other functional elements necessary to provide movement of at least one of the cutting member housing assembly and/or the cutting member receiving assembly.
  • Transport assembly may also comprise a controller configured to control at least one of speed, distance, elongated cutting member tension, or any other characteristics of the transport assembly.
  • a planar assembly may comprise a groove or slot suitable for receiving an edge of a laminated substrate assembly 302 to provide vertical stability.
  • a calibration assembly may determine an initial position for the cutting assembly along an adhesive seam of a laminated substrate. Additionally, adhesive seam may be located manually, and cutting assembly may be positioned manually.
  • Delaminated substrate assembly layers 602 , 604 , 606 may be any rigid or semi-rigid planar surface of glass, plastic, film, metal, an anti-reflective/anti-glare substrate, a touch panel, a glass substrate, a polarizing film substrate, an LCD, an electrode plane including a conductive coating (e.g., indium-tin oxide) substrate, another glass substrate, and/or another polarizing film substrate.
  • Substrate layers 602 , 604 may be different materials, different shapes, different thickness, and/or different sizes.
  • An adhesive layer 606 may be substantially removed between at least two layers (e.g. 602 , 604 of FIG. 6 ) of the delaminated laminated substrate assembly 600 . In some instances, at least a portion of an adhesive layer 606 may remain after separation, as shown.
  • an amount of adhesive may be removed from one or more layers of the laminated substrate assembly 302 upon separation. It is contemplated that one or more layers of the laminated substrate assembly 302 may contain an amount of adhesive not removed by the elongated cutting member. Removal of adhesive may be accomplished with water, alcohol, solvent, or any other substance suitable for removing the adhesive from the substrate layer. The material utilized for cleaning the substrate layer may be selected from any appropriate cleaning materials.
  • System 700 may comprise a substantially planar assembly 702 .
  • the substantially planar assembly may comprise a surface 704 for receiving a laminated substrate assembly and a separation assembly 706 .
  • the separation assembly 706 may further comprise an elongated cutting member 708 , a cutting member housing assembly 710 and a cutting member receiving assembly 712 suitable for receiving the elongated cutting member.
  • the cutting member housing assembly 710 may be suitable for containing and releasing the elongated cutting member 708 and the cutting member receiving assembly 712 may be suitable for receiving the elongated cutting member 708 .
  • System 700 may further comprise a control assembly 714 for controlling the separation assembly 704 .
  • Method 700 may comprise providing a planar assembly 802 and placing a laminated substrate assembly on a surface of the planar assembly 804 .
  • Method 800 may also comprise determining a position of an adhesive layer of the laminated substrate assembly 806 .
  • Method may further comprise providing an elongated cutting member housing assembly configured to house an amount of an elongated cuffing member 808 and providing an elongated cutting member receiving assembly configured to receive an amount of the elongated cutting member 810 .
  • Method may comprise positioning an amount of the elongated cutting substantially between two layers of a laminated substrate assembly along a length of the adhesive layer of the laminated substrate assembly 812 and transferring an amount of elongated cutting member from the cutting member housing assembly to the cutting member receiving assembly 814 . Transfer may be accomplished by rotating at least one of the cutting member housing assembly or the cutting member receiving assembly. Such rotation may draw the elongated cutting member along the length of the adhesive layer.
  • the amount of elongated cutting member is configured to remove at least a portion of an adhesive as the amount of elongated cutting member is transferred from the cutting member housing assembly to the cutting member receiving assembly.
  • Method 900 may comprise guiding a planar assembly along at least one guide rail coupled to the planar assembly 902 and heating a surface of the planar assembly 904 . Heating of a surface of the planar assembly may occur before, during or after the laminated substrate assembly has been placed on the surface of the planar assembly 904 .
  • Method may be implemented with method 800 and one or more steps of method 900 may be implemented before or after any step of method 800 .
  • Systems and apparatuses in accordance with various aspects of the present invention provide a system and method for dissembling laminated substrates.
  • the present invention may be described herein in terms of functional block components and various processing steps. It should be appreciated that such functional blocks may be realized by any number of hardware, firmware, and/or software components configured to perform the specified functions.
  • the present invention may employ various integrated circuit components, e.g., memory elements, digital signal processing elements, look-up tables, and the like, which may carry out a variety of functions under the control of one or more microprocessors or other control devices.
  • Such general techniques and components that are known to those skilled in the art are not described in detail herein.
  • the invention is frequently described herein as pertaining to displays composed of one or more substrates, it will be appreciated that the systems and methods described herein could also be applied to any substrates adhered with any adhesive including, but not limited to, a pressure sensitive adhesive.
  • Various embodiments of the present invention include one or more techniques described below relating to separating laminated substrates. Each of these techniques may be implemented using standard user interface techniques, such as standard graphical software programming or the like. Of course any programming language or environment could be used to implement the techniques described herein. Furthermore, the foregoing described embodiments according to the present invention may be conveniently implemented using conventional general purpose digital computers programmed according to the teachings of the present specification, as will be apparent to those skilled in the computer art. Appropriate software coding may readily be prepared by skilled programmers based on the teachings of the present disclosure, as will be apparent to those skilled in the software art.

Landscapes

  • Life Sciences & Earth Sciences (AREA)
  • Forests & Forestry (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Adhesive Tapes (AREA)
  • Laminated Bodies (AREA)

Abstract

An apparatus for separating a laminated substrate assembly comprises at least a substantially planar assembly, a cutting member housing assembly positioned on a first side of the substantially planar assembly, a cutting member receiving assembly positioned on a second side of the substantially planar assembly, substantially opposite from the first side of the planar assembly suitable for receiving an amount of the elongated cutting member. At least one of the cutting member housing assembly or the cutting member receiving assembly is configured to provide an amount of tension to the elongated cutting member as the elongated cutting member is released by the cutting member housing assembly or received by the cutting member receiving assembly, and the elongated cutting member is configured to remove an amount of adhesive from an adhesive layer of the laminated substrate assembly.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS
The present application is related to and claims the benefit of earliest available effective filing date(s) from the following listed application(s) (the “Related Applications”) (e.g., claims earliest available priority dates for other than provisional patent applications; claims benefits under 35 USC §119(e) for provisional patent applications), and incorporates by reference in its entirety all subject matter of the following listed application(s); the present application also claims the earliest available effective filing date(s) from, and also incorporates by reference in its entirety all subject matter of any and all parent, grandparent, great-grandparent, etc. applications of the Related Application(s) to the extent such subject matter is not inconsistent herewith:
    • 1. U.S. patent application entitled “ALIGNMENT SYSTEM AND METHOD THEREOF,” naming James D. Sampica as the first named inventor, sent via Express Mail Envelope Number EM 117 518 667 US, filed on Jan. 18, 2008, which is currently co-pending, or is an application of which a currently co-pending application is entitled to the benefit of the filing date.
    • 2. U.S. patent application entitled “SUBSTRATE LAMINATION SYSTEM AND METHOD,” naming James D. Sampica as the first named inventor, sent via Express Mail Envelope Number EM 117 518 596 US, filed on Jan. 18, 2008, which is currently co-pending, or is an application of which a currently co-pending application is entitled to the benefit of the filing date.
    • 3. U.S. patent application entitled “SUBSTRATE LAMINATION SYSTEM AND METHOD,” naming James D. Sampica as the first named inventor, sent via Express Mail Envelope Number EM 117 518 605 US, filed on Jan. 18, 2008, which is currently co-pending, or is an application of which a currently co-pending application is entitled to the benefit of the filing date.
    • 4. U.S. patent application entitled “SYSTEM AND METHOD FOR COMPLETING LAMINATION OF RIGID-TO-RIGID SUBSTRATES BY THE CONTROLLED APPLICATION OF PRESSURE,” naming James D. Sampica as the first named inventor, sent via Express Mail Envelope Number EM 117 518 640 US, filed on Jan. 18, 2008, which is currently co-pending, or is an application of which a currently co-pending application is entitled to the benefit of the filing date.
    • 5. U.S. patent application entitled “PLANARIZATION TREATMENT OF PRESSURE SENSITIVE ADHESIVE FOR RIGID-TO-RIGID SUBSTRATE LAMINATION,” naming James D. Sampica as the first named inventor, sent via Express Mail Envelope Number EM 117 518 653 US, filed on Jan. 18, 2008, which is currently co-pending, or is an application of which a currently co-pending application is entitled to the benefit of the filing date.
All subject matter of the Related Application and of any and all parent, grandparent, great-grandparent, etc. applications of the Related Applications is incorporated herein by reference to the extent such subject matter is not inconsistent herewith.
TECHNICAL FIELD
The present invention relates generally to laminated substrates. More specifically, the present invention relates to disassembling laminated substrates.
BACKGROUND
Laminated displays are generally constructed for deployment within potentially harsh environments. Features of these harsh environments are high and low ambient temperatures, dust, moisture, vibration, shock and the inevitable risk of abuse by users who are operating under pressure-packed conditions. These challenges can be especially difficult when designing the displays that provide critical user interface functions and also are exposed to a risk of damage. Furthermore, a display may acquire defects during the lamination process or may be damaged by the manufacturer, shipper or user during handling.
When a laminated display has been damaged, the display generally must be discarded and no component parts of the display may be re-utilized. This creates waste and increased expense in acquiring replacement laminated displays.
Consequently, a system and method for separating laminated displays while minimizing the introduction of anomalies to the display is desired.
SUMMARY
According to an embodiment, an apparatus for separating laminated substrates is described. Apparatus may comprise a substantially planar assembly, the substantially planar assembly comprising a plate assembly suitable for receiving a laminated substrate assembly and a guide assembly configured to guide the plate assembly in at least one direction, a cutting member housing assembly positioned on a first side of the substantially planar assembly suitable for containing an elongated cutting member and releasing an amount of the elongated cutting member and a cutting member receiving assembly positioned on a second side of the substantially planar assembly, substantially opposite from the first side of the planar assembly suitable for receiving an amount of the elongated cutting member. At least one of the cutting member housing assembly or the cutting member receiving assembly is configured to provide an amount of tension to the elongated cutting member as the elongated cutting member is released by the cutting member housing assembly or received by the cutting member receiving assembly and the elongated cutting member is configured to remove an amount of adhesive from an adhesive layer of the laminated substrate assembly positioned on a top surface of the plate assembly of the planar assembly as the amount of the elongated cutting member is transferred from the cutting member housing assembly to the cutting member receiving assembly.
According to an additional embodiment, a method for separating laminated substrates is described. Method may comprise providing a planar assembly, placing a laminated substrate assembly on a surface of the planar assembly, determining a position of an adhesive layer of the laminated substrate assembly, providing an elongated cutting member housing assembly configured to house an amount of an elongated cuffing member, providing an elongated cutting member receiving assembly configured to receive an amount of the elongated cutting member, positioning an amount of the elongated cutting substantially between two layers of a laminated substrate assembly along a length of the adhesive layer of the laminated substrate assembly, and transferring an amount of elongated cutting member from the cutting member housing assembly to the cutting member receiving assembly by rotating at least one of the cutting member housing assembly or the cutting member receiving assembly to draw the elongated cutting member along the length of the adhesive layer. The amount of elongated cutting member is configured to remove at least a portion of an adhesive as the amount of elongated cutting member is transferred from the cutting member housing assembly to the cutting member receiving assembly.
According to a further additional embodiment of the invention, a system for separating laminated substrates is described. System may comprise a substantially planar assembly. The substantially planar assembly may comprise a surface for receiving a laminated substrate assembly and a separation assembly. The separation assembly may further comprise an elongated cutting member, a cutting member housing assembly and a cutting member receiving assembly suitable for receiving the elongated cutting member. The cutting member housing assembly may be suitable for containing and releasing the elongated cutting member and the cutting member receiving assembly may be suitable for receiving the elongated cutting member. System may further comprise a control assembly for controlling the separation assembly.
The foregoing summary is illustrative only and is not intended to be in any way limiting. In addition to the illustrative aspects, embodiments, and features described above, further aspects, embodiments, and features will become apparent by reference to the drawings and the following detailed description.
BRIEF DESCRIPTION OF THE DRAWINGS
The numerous objects and advantages of the present invention may be better understood by those skilled in the art by reference to the accompanying figures in which:
FIG. 1 is an isometric view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention;
FIG. 2 is an additional isometric view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention;
FIG. 3 is a further additional isometric view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention;
FIG. 4 is a side view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention;
FIG. 5 is a top view of an apparatus for separating laminated substrates according to an exemplary embodiment of the present invention;
FIG. 6 is an isometric illustration of laminated substrates separated via the apparatus for separating laminated substrates according to an exemplary embodiment of the present invention; and
FIG. 7 is a block diagram of a system for separating laminated substrates according to an exemplary embodiment of the present invention
FIG. 8 is a flow diagram of a method for separating laminated substrates according to an exemplary embodiment of the present invention; and
FIG. 9 is an additional flow diagram of a method for separating laminated substrates according to an exemplary embodiment of the present invention.
DETAILED DESCRIPTION
In the following detailed description, reference is made to the accompanying drawings, which form a part hereof. In the drawings, similar symbols typically identify similar components, unless context dictates otherwise. The illustrative embodiments described in the detailed description, drawings, and claims are not meant to be limiting. Other embodiments may be utilized, and other changes may be made, without departing from the spirit or scope of the subject matter presented here.
Referring generally to FIGS. 1-5, an apparatus 100 for separating laminated substrates is described. Apparatus 100 may comprise a substantially planar assembly 102, the substantially planar assembly 102 comprising a plate assembly 104 suitable for receiving a laminated substrate assembly and a guide assembly 106 configured to guide the plate assembly 104 in at least one direction, a cutting member housing assembly 108 positioned on a first side of the substantially planar assembly 102 suitable for containing an elongated cutting member 110 and releasing an amount of the elongated cutting member 110 and a cutting member receiving assembly 112 positioned on a second side of the substantially planar assembly 102, substantially opposite from the first side of the planar assembly 102 suitable for receiving an amount of the elongated cutting member 110. At least one of the cutting member housing assembly 108 or the cutting member receiving assembly 112 is configured to provide an amount of tension to the elongated cutting member 110 as the elongated cutting member 110 is released by the cutting member housing assembly 108 or received by the cutting member receiving assembly 112 and the elongated cutting member 110 is configured to remove an amount of adhesive from an adhesive layer of the laminated substrate assembly positioned on the top surface of the plate assembly 104 of the planar assembly 102 as the amount of the elongated cutting member 110 is transferred from the cutting member housing assembly 108 to the cutting member receiving assembly 112.
Referring to FIG. 3, an example of a laminated substrate assembly 302 is shown on an apparatus 100 for separating a laminated substrate assembly. A “substrate” as used herein may further refer to any rigid or semi-rigid planar surface of glass, plastic, film, and/or metal coated with an adhesive. A laminated substrate assembly 302 may comprise an anti-reflective/anti-glare substrate, a touch panel, a glass substrate, a polarizing film substrate, an LCD, an electrode plane including a conductive coating (e.g., indium-tin oxide) substrate, another glass substrate, and/or another polarizing film substrate. Laminated substrate assembly 302 may be, for example, a conventional display comprising, for example, at least two substrates between which the liquid crystal material is disposed and a third substrate adhered to a top layer of the conventional display. Lines of electrodes may be patterned onto the first and second substrates. A third substrate may be an optically bonded safety/filter glass or touch screen. Adhesive layer may composed of pressure sensitive adhesive, or any adhesive that forms a bond when pressure is applied to marry the adhesive with the adherend. It is contemplated, however, that adhesive layer may be composed of a structural adhesive, i.e., any adhesive that hardens via processes such as evaporation of solvent or water (white glue), reaction with radiation (dental adhesives), chemical reaction (two part epoxy), or cooling, or any combination of structural and pressure sensitive adhesive. The adhesive layer may be composed of have a thickness, for example, from a range of about 20 microns to 3000 microns.
Pressure sensitive adhesive (PSA) may be any adhesive suitable for forming a bond when pressure is applied to engage the adhesive with the adherend. The pressure-sensitive adhesive may be a viscoelastic material utilized in this study, energy dissipation through large-scale bridging effects as well as time-dependent strain-rate effects must be considered.
In one embodiment, as illustrated in FIGS. 1-5, a plate assembly 104 of the planar assembly 102 may be a substantially horizontal surface (e.g. table top). However, it is contemplated that additional embodiments may include a planar assembly 102 including a plate assembly 104 that is substantially convexly or concavely curved (e.g. semi-spherical) or arced, may undulate (e.g. sinusoidally), may be configured to receive corner portions formed at any angle and/or may be customized to receive laminated substrate assemblies formed in any shape or abstract formation. Planar assembly 102 may be composed substantially of metal, metal alloy, heat resistive plastic, ceramic, silicone or any other natural or synthetic material capable of forming a substantially smooth, flat surface. Planar assembly plate assembly 104 may comprise at least one guide marker 114 (e.g. a rectangular outline) formed on or imbedded into a top surface of the plate assembly 104. Guide marker 114 may provide placement or movement guidance for displays of known or predetermined size and shape. Plate assembly top surface may comprise a plurality of guide markers 114 outlining a plurality of laminated substrate display sizes and/or shapes.
The plate assembly 104 of the planar assembly 102 may be configured to receive an amount of heat from a heat source. The heat source is a uniform heat source configured to uniformly heat a region of the plate assembly 104 of the planar assembly 102. For instance, the planar assembly 102 may comprise a plurality of heating mechanisms configured provide substantially uniform heating of the plate assembly 104 of the planar assembly 102. A laminated substrate assembly 302 placed on the plate assembly 104 of the planar assembly 102 may receive heat from the heated plate assembly 104. Heating of the plate assembly 104 of the planar assembly 102, and thus, the laminated substrate assembly 302 may be to a temperature not lower than the softening temperature of the adhesive utilized to bond the substrates.
Guide assembly 106 may be a rail or post along which the plate assembly 104 may glide or move along. Guide assembly 106 may be manually operated or motorized as desired, and may provide substantially linear movement of the plate assembly 104 of the planar assembly 102. In additional embodiments, guide assembly 106 may be configured to match the shape or path determined by the shape of the plate assembly 104.
The elongated cutting member 110 may be a wire or any other such cylindrical, flat and/or otherwise shaped, elongated string of drawn material such as metal, metal alloy, plastic, silicone or any other natural or synthetic material comprising an appropriate tensile strength and suitable to be elongated into string or wire form. The metals suitable for forming an elongated cutting member 110 may include platinum, silver, iron, copper, aluminum and gold.
The cutting member housing assembly 108 may be a first hub. In one embodiment, first hub may be substantially cylindrical. For instance, cutting member housing assembly 108 may be a flanged cylinder, reel or other such housing for an amount of an elongated cutting member 110 comprising a flange 118 as shown in FIG. 2, or an unflanged cylinder, reel or other such housing for an amount of an elongated cutting member 110 and on which the elongated cutting member 110 may be wound. However, any shape may be utilized to form the first hub. According to at least one embodiment, at least a portion of the elongated cutting member 110 may be wrapped substantially about the first hub. Cutting member housing assembly 108 may be motorized or manually operated. Cutting member housing assembly 108 may rotate along an axis to release an amount of the elongated cutting member 110 as necessary to maintain elongated cutting member 110 at a desired tautness.
The cutting member receiving assembly 112 may be a second hub configured to receive at least a portion of the elongated cutting member 110. In one embodiment, second hub may be substantially cylindrical. For instance, cutting member receiving assembly 112 may be a flanged or unflanged cylinder or reel on which the elongated cutting member 110 may be wound. However, any shape may be utilized to form the second hub. At least a portion of an elongated cutting member 110 may be configured to wrap substantially about the second hub after at least a portion of the adhesive has been removed from the laminated substrate assembly 302. Cutting member receiving assembly 112 may be motorized or manually operated. Cutting member receiving assembly 112 may rotate along an axis to receive an amount of the elongated cutting member 110 as necessary to maintain elongated cutting member 110 at a desired tautness.
The apparatus 100 may further comprise a calibration assembly 116 configured to calibrate a zero point relative to a top surface of the plate assembly 104 of the planar assembly 102. It is contemplated that a laminated assembly adhesive joint may be at any height relative to a top surface of the plate assembly 104 of the planar assembly 102 when the laminated assembly 302 (FIG. 3) is placed on the top surface of the plate assembly 104 of the planar assembly 102. A calibration assembly 116 may be configured to mark the top surface 104 of the planar assembly 102 as a zero distance point. Calibration assembly 116 may also receive an input relating to a distance from the top surface of the plate assembly 104 (e.g. the zero point) of the planar assembly 102 to the adhesive layer of the laminated substrate assembly 302. Distance input may be manually entered into, for example, a control of the calibration assembly 116 via a keypad or other such device suitable for entering numeric values. The calibration assembly 116 may also be connected to a database of known laminated substrate assembly thicknesses, including a thickness of any individual components of the laminated substrate assembly 302. Calibration assembly 116 may then determine a set point for the elongated cutting member 110 above the top surface 104 of the planar assembly 102. Set point may be, for example, at a distance above the zero point, designated by distance 122 in FIG. 1 and FIG. 4, corresponding with the position of the adhesive layer of the laminated substrate assembly 302 above the top surface 104 of the planar assembly 102. Calibration assembly 116 may be electrically connected to at least one of the cutting member housing assembly 108 and the cutting member receiving assembly 112, and thus may be comprised of at least two separate calibration components (each designated as 116). Each of the calibration assembly 116 components may raise or lower at least a portion of the elongated cutting member 110. A database of known laminated substrate assembly component thicknesses may be utilized by the calibration assembly 116 to determine a set point for the elongated cutting member 110 at a distance above the zero point corresponding with the thickness of any laminated assembly components located below the adhesive layer of the laminated substrate assembly 302 plus any additional amount as desired by an operator.
The apparatus 100 may further comprise an edge assembly (not shown) configured to attach to a top surface of the plate assembly 104 of the planar assembly 102 and guide the laminated substrate in a direction substantially orthogonal to the elongated cutting member 110. Edge assembly may facilitate the application of uniform force to the laminated substrate assembly 302. For instance, as a laminated substrate assembly 302 travels along the planar assembly 102 in a direction orthogonal to the motion of the elongated cutting member 110, the motion may be substantially uniform across the leading edge of the laminated substrate assembly 302 by force applied to a trailing edge of the laminated substrate assembly via the edge assembly.
In an additional embodiment, apparatus 100 may be configured to remove a vertically positioned display. For instance, a planar assembly may comprise a vertical stability assembly configured to apply an amount of pressure to at least two surfaces of a laminated substrate assembly 302 to provide vertical stability for the laminated substrate assembly 302. Cutting assembly may be configured to traverse through an adhesive layer while the laminated substrate assembly 302 is vertically positioned and stationary. In this embodiment, a cutting member housing assembly and a cutting member receiving assembly may be as described above and in FIGS. 1-5 configured to house and receive an elongated cutting member (e.g. a wire), and may further comprise a transport assembly configured to raise or lower the cutting member housing assembly and the cutting member receiving assembly as necessary to traverse through the laminated substrate along the adhesive layer. In some instances, transport assembly may be individually or simultaneously controlled. Transport mechanism may be manual, hydraulic, motorized or comprise any other functional elements necessary to provide movement of at least one of the cutting member housing assembly and/or the cutting member receiving assembly. Transport assembly may also comprise a controller configured to control at least one of speed, distance, elongated cutting member tension, or any other characteristics of the transport assembly. In a further additional embodiment, a planar assembly may comprise a groove or slot suitable for receiving an edge of a laminated substrate assembly 302 to provide vertical stability. A calibration assembly may determine an initial position for the cutting assembly along an adhesive seam of a laminated substrate. Additionally, adhesive seam may be located manually, and cutting assembly may be positioned manually.
Referring to FIG. 6, an example of a delaminated substrate assembly 600 that has been delaminated via apparatus 100 is shown. Delaminated substrate assembly layers 602, 604, 606 may be any rigid or semi-rigid planar surface of glass, plastic, film, metal, an anti-reflective/anti-glare substrate, a touch panel, a glass substrate, a polarizing film substrate, an LCD, an electrode plane including a conductive coating (e.g., indium-tin oxide) substrate, another glass substrate, and/or another polarizing film substrate. Substrate layers 602, 604 may be different materials, different shapes, different thickness, and/or different sizes. An adhesive layer 606 may be substantially removed between at least two layers (e.g. 602, 604 of FIG. 6) of the delaminated laminated substrate assembly 600. In some instances, at least a portion of an adhesive layer 606 may remain after separation, as shown.
In additional embodiments, an amount of adhesive may be removed from one or more layers of the laminated substrate assembly 302 upon separation. It is contemplated that one or more layers of the laminated substrate assembly 302 may contain an amount of adhesive not removed by the elongated cutting member. Removal of adhesive may be accomplished with water, alcohol, solvent, or any other substance suitable for removing the adhesive from the substrate layer. The material utilized for cleaning the substrate layer may be selected from any appropriate cleaning materials.
Referring to FIG. 7, a system 700 for separating a laminated substrate assembly is shown. System 700 may comprise a substantially planar assembly 702. The substantially planar assembly may comprise a surface 704 for receiving a laminated substrate assembly and a separation assembly 706. The separation assembly 706 may further comprise an elongated cutting member 708, a cutting member housing assembly 710 and a cutting member receiving assembly 712 suitable for receiving the elongated cutting member. The cutting member housing assembly 710 may be suitable for containing and releasing the elongated cutting member 708 and the cutting member receiving assembly 712 may be suitable for receiving the elongated cutting member 708. System 700 may further comprise a control assembly 714 for controlling the separation assembly 704.
Referring to FIG. 8, a method 800 for separating a laminated substrate assembly is shown. Method 700 may comprise providing a planar assembly 802 and placing a laminated substrate assembly on a surface of the planar assembly 804. Method 800 may also comprise determining a position of an adhesive layer of the laminated substrate assembly 806. Method may further comprise providing an elongated cutting member housing assembly configured to house an amount of an elongated cuffing member 808 and providing an elongated cutting member receiving assembly configured to receive an amount of the elongated cutting member 810. Method may comprise positioning an amount of the elongated cutting substantially between two layers of a laminated substrate assembly along a length of the adhesive layer of the laminated substrate assembly 812 and transferring an amount of elongated cutting member from the cutting member housing assembly to the cutting member receiving assembly 814. Transfer may be accomplished by rotating at least one of the cutting member housing assembly or the cutting member receiving assembly. Such rotation may draw the elongated cutting member along the length of the adhesive layer. The amount of elongated cutting member is configured to remove at least a portion of an adhesive as the amount of elongated cutting member is transferred from the cutting member housing assembly to the cutting member receiving assembly.
Referring to FIG. 9, a flow diagram representing an additional method 900 for separating a laminated substrate assembly is shown. Method 900 may comprise guiding a planar assembly along at least one guide rail coupled to the planar assembly 902 and heating a surface of the planar assembly 904. Heating of a surface of the planar assembly may occur before, during or after the laminated substrate assembly has been placed on the surface of the planar assembly 904. Method may be implemented with method 800 and one or more steps of method 900 may be implemented before or after any step of method 800.
Systems and apparatuses in accordance with various aspects of the present invention provide a system and method for dissembling laminated substrates. In this regard, the present invention may be described herein in terms of functional block components and various processing steps. It should be appreciated that such functional blocks may be realized by any number of hardware, firmware, and/or software components configured to perform the specified functions. For example, the present invention may employ various integrated circuit components, e.g., memory elements, digital signal processing elements, look-up tables, and the like, which may carry out a variety of functions under the control of one or more microprocessors or other control devices. Such general techniques and components that are known to those skilled in the art are not described in detail herein. Furthermore, although the invention is frequently described herein as pertaining to displays composed of one or more substrates, it will be appreciated that the systems and methods described herein could also be applied to any substrates adhered with any adhesive including, but not limited to, a pressure sensitive adhesive.
It is understood that the specific order or hierarchy of steps in the foregoing disclosed methods are examples of exemplary approaches. Based upon design preferences, it is understood that the specific order or hierarchy of steps in the method may be rearranged while remaining within the scope of the present invention. The accompanying method claims present elements of the various steps in a sample order, and are not meant to be limited to the specific order or hierarchy presented.
Various embodiments of the present invention include one or more techniques described below relating to separating laminated substrates. Each of these techniques may be implemented using standard user interface techniques, such as standard graphical software programming or the like. Of course any programming language or environment could be used to implement the techniques described herein. Furthermore, the foregoing described embodiments according to the present invention may be conveniently implemented using conventional general purpose digital computers programmed according to the teachings of the present specification, as will be apparent to those skilled in the computer art. Appropriate software coding may readily be prepared by skilled programmers based on the teachings of the present disclosure, as will be apparent to those skilled in the software art.
It is believed that the present invention and many of its attendant advantages will be understood by the foregoing description, and it will be apparent that various changes may be made in the form, construction, and arrangement of the components thereof without departing from the scope and spirit of the invention or without sacrificing all of its material advantages. The form herein before described being merely an explanatory embodiment thereof, it is the intention of the following claims to encompass and include such changes.

Claims (15)

What is claimed is:
1. An apparatus for separating a laminated substrate assembly comprising:
a planar assembly, the planar assembly comprising a plate assembly for receiving a laminated substrate assembly and a guide assembly configured to guide the plate assembly in at least one direction;
an elongated cutting member;
a cutting member housing assembly positioned on a first side of the planar assembly suitable for containing the elongated cutting member and releasing an amount of the elongated cutting member; and
a cutting member receiving assembly positioned on a second side of the planar assembly, substantially opposite from the first side of the planar assembly suitable for receiving an amount of the elongated cutting member; and
a heating assembly coupled to the planar assembly configured to uniformly heat a surface of the plate assembly;
wherein at least one of the cutting member housing assembly or the cutting member receiving assembly is configured to provide an amount of tension to an amount of the elongated cutting member as the amount of elongated cutting member is released by the cutting member housing assembly or received by the cutting member receiving assembly, and the elongated cutting member is configured to remove an amount of adhesive from an adhesive layer of the laminated substrate assembly positioned on a top surface of the plate assembly of the planar assembly as the amount of the elongated cutting member is transferred from the cutting member housing assembly to the cutting member receiving assembly.
2. The apparatus of claim 1, wherein the guide assembly guides the plate assembly in a substantially forward direction as the amount of the elongated cutting member is transferred from the cutting member housing assembly to the cutting member receiving assembly.
3. The apparatus of claim 1, wherein the elongated cutting member is a cylindrical shaped member.
4. The apparatus of claim 1, wherein the cutting member housing assembly is a first hub.
5. The apparatus of claim 4, wherein at least a portion of the elongated cutting member is wrapped about the first hub.
6. The apparatus of claim 5, wherein the first hub is configured to provide an amount of tension for the elongated cutting member.
7. The apparatus of claim 1, wherein the cutting member receiving assembly is a second hub configured to receive at least a portion of the elongated cutting member.
8. The apparatus of claim 7, wherein the second hub is configured to provide an amount of tension for the elongated cutting member.
9. The apparatus of claim 7, wherein the at least a portion of the elongated cutting member is configured to wrap about the second hub after at least a portion of the adhesive has been removed from the laminated substrate assembly.
10. The apparatus of claim 1, wherein the planar assembly is configured to align the laminated substrate in a direction orthogonal to the elongated cutting member.
11. The apparatus of claim 1, further comprising a calibration assembly configured to calibrate a zero point for the separation assembly relative to the planar assembly.
12. The apparatus of claim 1, further comprising a plate assembly configured to attach to the planar assembly and guide the laminated substrate in a direction orthogonal to the elongated cutting member.
13. The apparatus of claim 1, further comprising a controller for controlling at least one of the speed and tension of the elongated cutting member.
14. An apparatus for separating a laminated substrate assembly comprising:
a planar assembly, the planar assembly comprising a plate assembly for receiving a laminated substrate assembly and a guide assembly configured to guide the plate assembly in at least one direction;
a cutting member housing assembly positioned on a first side of the planar assembly suitable for containing an elongated cutting member and releasing an amount of the elongated cutting member; and
a cutting member receiving assembly positioned on a second side of the planar assembly, substantially opposite from the first side of the planar assembly suitable for receiving an amount of the elongated cutting member;
a heating assembly coupled to the planar assembly and configured to uniformly heat a surface of the plate assembly;
wherein at least one of the cutting member housing assembly or the cutting member receiving assembly is configured to provide an amount of tension to an amount of the elongated cutting member as the amount of elongated cutting member is released by the cutting member housing assembly or received by the cutting member receiving assembly, and the elongated cutting member is configured to remove an amount of adhesive from an adhesive layer of the laminated substrate assembly positioned on a top surface of the plate assembly of the planar assembly as the amount of the elongated cutting member is transferred from the cutting member housing assembly to the cutting member receiving assembly.
15. The apparatus of claim 14, further comprising the elongated cutting member;
wherein the elongated cutting member is a cylindrical-shaped cutting member.
US12/009,372 2005-08-30 2008-01-18 System and method for disassembling laminated substrates Active 2030-09-03 US8118075B2 (en)

Priority Applications (16)

Application Number Priority Date Filing Date Title
US12/009,372 US8118075B2 (en) 2008-01-18 2008-01-18 System and method for disassembling laminated substrates
US12/009,482 US8936057B2 (en) 2005-08-30 2008-01-18 Substrate lamination system and method
EP09702309.7A EP2243054A4 (en) 2008-01-18 2009-01-15 Substrate lamination system and method
JP2010543255A JP5431364B2 (en) 2008-01-18 2009-01-15 Substrate stacking system and method
KR1020107017278A KR101625880B1 (en) 2008-01-18 2009-01-15 Substrate lamination system and method
EP16188276.6A EP3135490B1 (en) 2008-01-18 2009-01-15 Substrate lamination apparatus
PCT/US2009/031151 WO2009091923A2 (en) 2008-01-18 2009-01-15 Substrate lamination system and method
KR1020167013740A KR101763710B1 (en) 2008-01-18 2009-01-15 Substrate lamination system and method
EP14161363.8A EP2749412B1 (en) 2008-01-18 2009-01-15 Substrate lamination method
CN200980107294.5A CN101971080B (en) 2008-01-18 2009-01-15 Substrate lamination system and method
CN201510005057.5A CN104765168B (en) 2008-01-18 2009-01-15 Substrate laminating apparatus and to Barebone
JP2013251126A JP5762516B2 (en) 2008-01-18 2013-12-04 Substrate stacking system and method
US14/270,563 US9638944B1 (en) 2008-01-18 2014-05-06 Systems and methods for substrate lamination
JP2015116688A JP5869171B2 (en) 2008-01-18 2015-06-09 Substrate stacking system and method
JP2015116716A JP5869172B2 (en) 2008-01-18 2015-06-09 Substrate stacking system and method
JP2016001165A JP6186452B2 (en) 2008-01-18 2016-01-06 Substrate stacking system and method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/009,372 US8118075B2 (en) 2008-01-18 2008-01-18 System and method for disassembling laminated substrates

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US12/009,393 Continuation-In-Part US8137498B2 (en) 2005-08-30 2008-01-18 System and method for completing lamination of rigid-to-rigid substrates by the controlled application of pressure

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US12/009,375 Continuation-In-Part US8691043B2 (en) 2005-08-30 2008-01-18 Substrate lamination system and method

Publications (2)

Publication Number Publication Date
US20090183615A1 US20090183615A1 (en) 2009-07-23
US8118075B2 true US8118075B2 (en) 2012-02-21

Family

ID=40875399

Family Applications (1)

Application Number Title Priority Date Filing Date
US12/009,372 Active 2030-09-03 US8118075B2 (en) 2005-08-30 2008-01-18 System and method for disassembling laminated substrates

Country Status (1)

Country Link
US (1) US8118075B2 (en)

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20090120585A1 (en) * 2005-08-30 2009-05-14 Sampica James D Substrate lamination system and method
US20090186218A1 (en) * 2008-01-18 2009-07-23 Sampica James D Planarization treatment of pressure sensitive adhesive for rigid-to-rigid substrate lamination
US20100154992A1 (en) * 2008-12-22 2010-06-24 Feinstein Casey J Layer-Specific Energy Distribution Delamination
US20110180218A1 (en) * 2008-11-20 2011-07-28 E.I. Du Pont De Nemours And Company Semi-automated reworkability process for de-bonding a display
US8261804B1 (en) * 2011-10-28 2012-09-11 Meicer Semiconductor Inc. IC layers separator
US20120263956A1 (en) * 2009-10-16 2012-10-18 Sony Chemical & Information Device Corporation Display, manufacturing method therefor and transparent resin charging material
US8486535B1 (en) 2010-05-24 2013-07-16 Rockwell Collins, Inc. Systems and methods for adherable and removable thin flexible glass
US8540002B2 (en) 2005-08-30 2013-09-24 Rockwell Collins, Inc. System and method for completing lamination of rigid-to-rigid substrates by the controlled application of pressure
US8647727B1 (en) 2012-06-29 2014-02-11 Rockwell Colllins, Inc. Optical assembly with adhesive layers configured for diffusion
US20140130987A1 (en) * 2012-11-09 2014-05-15 Boe (Hebei) Mobile Display Technology Co., Ltd. Film stripping mechanism
US8888953B2 (en) 2012-10-17 2014-11-18 Saxum LLC Method and apparatus for display screen shield replacement
US20140338828A1 (en) * 2013-05-14 2014-11-20 Samsung Display Co., Ltd. Substrate separation apparatus and method
US20150197024A1 (en) * 2014-01-15 2015-07-16 Southwest Research Institute Method And Apparatus To Propagate Crack Growth In A Workpiece
US9254636B2 (en) 2013-09-24 2016-02-09 Apple Inc. Display module reworkability
US9384586B1 (en) 2013-04-05 2016-07-05 Rockwell Collins, Inc. Enhanced flight vision system and method with radar sensing and pilot monitoring display
US20160195968A1 (en) * 2015-01-06 2016-07-07 Boe Technology Group Co., Ltd. Method and system for separating touch panel from display module
US20160279862A1 (en) * 2015-03-27 2016-09-29 Intel Corporation Hidden feature for accessing or repairing mobile devices
US20160375600A1 (en) * 2015-06-29 2016-12-29 Igor Markovsky Joint cutting in a device
US9638944B1 (en) 2008-01-18 2017-05-02 Rockwell Collins, Inc. Systems and methods for substrate lamination
US9733349B1 (en) 2007-09-06 2017-08-15 Rockwell Collins, Inc. System for and method of radar data processing for low visibility landing applications
US9939526B2 (en) 2007-09-06 2018-04-10 Rockwell Collins, Inc. Display system and method using weather radar sensing
US9981460B1 (en) 2014-05-06 2018-05-29 Rockwell Collins, Inc. Systems and methods for substrate lamination
US20180354251A1 (en) * 2015-10-30 2018-12-13 Corning Incorporated Methods for processing a first substrate bonded to a second substrate
US10228460B1 (en) 2016-05-26 2019-03-12 Rockwell Collins, Inc. Weather radar enabled low visibility operation system and method
US10353068B1 (en) 2016-07-28 2019-07-16 Rockwell Collins, Inc. Weather radar enabled offshore operation system and method
US10705201B1 (en) 2015-08-31 2020-07-07 Rockwell Collins, Inc. Radar beam sharpening system and method
US10928510B1 (en) 2014-09-10 2021-02-23 Rockwell Collins, Inc. System for and method of image processing for low visibility landing applications
US11548084B2 (en) * 2016-03-15 2023-01-10 Saint-Gobain Placo Method and device for cutting a plate or panel of porous construction material

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8691043B2 (en) * 2005-08-30 2014-04-08 Rockwell Collins, Inc. Substrate lamination system and method
TW200934662A (en) * 2007-12-28 2009-08-16 Du Pont Method for reworking adhesively bonded liquid crystal displays
WO2011030480A1 (en) * 2009-09-14 2011-03-17 シャープ株式会社 Apparatus and method for peeling adhesive film
US8411235B1 (en) 2010-03-16 2013-04-02 Rockwell Collins, Inc. Displays for three-dimensional imaging
US8419496B1 (en) 2010-03-18 2013-04-16 Rockwell Collins, Inc. Display panel alignment system
US8576370B1 (en) 2010-06-30 2013-11-05 Rockwell Collins, Inc. Systems and methods for nonplanar laminated assemblies
US8643260B1 (en) 2011-09-02 2014-02-04 Rockwell Collins, Inc. Systems and methods for display assemblies having printed masking
CN103676282A (en) * 2013-12-23 2014-03-26 合肥京东方光电科技有限公司 Touch screen and display screen separation device and method
US9517615B2 (en) * 2015-04-21 2016-12-13 The Boeing Company System and method for automated backing film removal
CN104932129B (en) * 2015-07-17 2017-11-17 武汉华星光电技术有限公司 A kind of polarizer stripping device
US11177153B2 (en) * 2018-03-20 2021-11-16 Chengdu Eswin Sip Technology Co., Ltd. Method of debonding work-carrier pair with thin devices
US11260647B2 (en) * 2020-07-07 2022-03-01 Gulfstream Aerospace Corporation Apparatus and method for decoupling an element that is bonded to a surface by adhesive
KR102476313B1 (en) * 2021-02-04 2022-12-13 (주)미래컴퍼니 Protective film peeling apparatus and method using the same

Citations (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3851758A (en) 1972-04-26 1974-12-03 Ibm Semiconductor chip fixture
JPH01210328A (en) 1988-02-19 1989-08-23 Honda Motor Co Ltd Film positioning method in vacuum laminating device and its device
WO1993005634A1 (en) 1991-09-06 1993-03-18 American Telephone & Telegraph Company SURFACE MOUNT ASSEMBLY OF DEVICES USING AdCon INTERCONNECTIONS
JPH05200880A (en) 1991-08-09 1993-08-10 Morton Internatl Inc Conveyor type vacuum applicator and its method
JPH05293895A (en) 1992-04-20 1993-11-09 Dainippon Printing Co Ltd Device and method for laminated molding with vacuum press
JPH0651484A (en) 1992-06-02 1994-02-25 E I Du Pont De Nemours & Co Sheet separating device
US5566840A (en) 1993-11-12 1996-10-22 Multiline International Europa L.P. Device for aligning printed circuit boards and pattern carriers
US5592288A (en) 1995-04-28 1997-01-07 Rockwell International Corp. Method and apparatus for pre-assembling optical components for use with liquid crystal displays
JPH0957779A (en) 1995-08-22 1997-03-04 Meiki Co Ltd Vacuum multistage lamination device
JPH10156853A (en) 1996-11-29 1998-06-16 Meiki Co Ltd Vacuum multiple laminating machine
JPH10244589A (en) 1997-03-06 1998-09-14 Fuji Electric Co Ltd Laminating device
US5918517A (en) * 1990-07-27 1999-07-06 Societe Croma Method and apparatus for cutting blocks and panels of cellular plastic
US5950512A (en) * 1996-10-11 1999-09-14 Gary D. Fields Apparatus to make building blocks for blockwork domed structures, and method and domed structure
EP0711103B1 (en) 1991-09-06 2000-03-08 AT&T Corp. Surface mount assembly of devices using AdCon interconnections
JP2000141388A (en) 1998-11-06 2000-05-23 Nichigo Morton Co Ltd Method for laminating
US6388724B1 (en) 2000-05-02 2002-05-14 Rockwell Collins, Inc. Apparatus having a platen with pins and standoffs, used to laminate an LCD to other optical components using silicone gel
US20030089214A1 (en) * 1998-11-05 2003-05-15 Ngk Insulators, Ltd. Cutting apparatus for ceramic green bodies
US6614057B2 (en) 2001-02-07 2003-09-02 Universal Display Corporation Sealed organic optoelectronic structures
US20030180528A1 (en) 2002-03-22 2003-09-25 Eastman Kodak Company Cellulose film with anti-blocking properties
US6681668B1 (en) * 2000-08-25 2004-01-27 Steven John Smirle Device and process for thermally cutting a moving web of textile material
JP2004233590A (en) 2003-01-29 2004-08-19 Kyocera Corp Pressing device
US6803245B2 (en) 2001-09-28 2004-10-12 Osram Opto Semiconductors Gmbh Procedure for encapsulation of electronic devices
US6832538B1 (en) * 2000-01-06 2004-12-21 Ber-Fong Hwang Foam sponge cutting apparatus with both vertical and horizontal cutting devices
US20050126679A1 (en) 2003-12-13 2005-06-16 Kwang-Jin Kim Apparatus and method for fabricating liquid crystal display
US6984545B2 (en) 2002-07-22 2006-01-10 Micron Technology, Inc. Methods of encapsulating selected locations of a semiconductor die assembly using a thick solder mask
US6998648B2 (en) 2003-08-25 2006-02-14 Universal Display Corporation Protected organic electronic device structures incorporating pressure sensitive adhesive and desiccant
JP2006218658A (en) 2005-02-08 2006-08-24 Fuji Electric Holdings Co Ltd Vacuum laminator and vacuum lamination method
US20060245171A1 (en) 2005-04-29 2006-11-02 Sok-San Kim Plasma display module
JP2006334912A (en) 2005-06-01 2006-12-14 Dainippon Printing Co Ltd Lamination device
JP2007206559A (en) 2006-02-03 2007-08-16 Yamaichi Electronics Co Ltd Method for removing film for liquid crystal display panel
US7273403B2 (en) 2001-12-27 2007-09-25 Kabushiki Kaisha Toshiba Method of manufacturing flat display panels of different sizes from a common base substrate
US20070297736A1 (en) 2006-06-27 2007-12-27 3M Innovative Properties Company Rigid optical laminates and methods of forming the same
US7381110B1 (en) 2005-08-30 2008-06-03 Rockwell Collins, Inc. Process for applying a protective cover on an organic light-emitting diode using a liquid adhesive
JP2008238607A (en) 2007-03-28 2008-10-09 Tafu:Kk Thin-film type laminating apparatus and lamination method using the same
US7435311B1 (en) 2005-08-30 2008-10-14 Rockwell Collins, Inc. Panel-to-panel lamination method for improved uniformity
US7452258B1 (en) 2005-08-30 2008-11-18 Rockwell Collins, Inc. Method of sealing OLED cover with liquid adhesive
US20090120585A1 (en) 2005-08-30 2009-05-14 Sampica James D Substrate lamination system and method
US20090120572A1 (en) 2005-08-30 2009-05-14 Sampica James D Substrate lamination system and method
US20090126872A1 (en) 2005-08-30 2009-05-21 Sampica James D System and method for completing lamination of rigid-to-rigid substrates by the controlled application of pressure
US20090183381A1 (en) 2008-01-18 2009-07-23 Sampica James D Alignment system and method thereof
US20090186218A1 (en) 2008-01-18 2009-07-23 Sampica James D Planarization treatment of pressure sensitive adhesive for rigid-to-rigid substrate lamination

Patent Citations (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3851758A (en) 1972-04-26 1974-12-03 Ibm Semiconductor chip fixture
JPH01210328A (en) 1988-02-19 1989-08-23 Honda Motor Co Ltd Film positioning method in vacuum laminating device and its device
US5918517A (en) * 1990-07-27 1999-07-06 Societe Croma Method and apparatus for cutting blocks and panels of cellular plastic
JPH05200880A (en) 1991-08-09 1993-08-10 Morton Internatl Inc Conveyor type vacuum applicator and its method
EP0556351B1 (en) 1991-09-06 1995-06-21 AT&T Corp. SURFACE MOUNT ASSEMBLY OF DEVICES USING AdCon INTERCONNECTIONS
EP0711103B1 (en) 1991-09-06 2000-03-08 AT&T Corp. Surface mount assembly of devices using AdCon interconnections
WO1993005634A1 (en) 1991-09-06 1993-03-18 American Telephone & Telegraph Company SURFACE MOUNT ASSEMBLY OF DEVICES USING AdCon INTERCONNECTIONS
JPH05293895A (en) 1992-04-20 1993-11-09 Dainippon Printing Co Ltd Device and method for laminated molding with vacuum press
JPH0651484A (en) 1992-06-02 1994-02-25 E I Du Pont De Nemours & Co Sheet separating device
US5678303A (en) * 1992-06-02 1997-10-21 Sterling Diagnostic Imaging, Inc. Apparatus for separating film from x-ray cassettes
US5566840A (en) 1993-11-12 1996-10-22 Multiline International Europa L.P. Device for aligning printed circuit boards and pattern carriers
US5592288A (en) 1995-04-28 1997-01-07 Rockwell International Corp. Method and apparatus for pre-assembling optical components for use with liquid crystal displays
JPH0957779A (en) 1995-08-22 1997-03-04 Meiki Co Ltd Vacuum multistage lamination device
US5950512A (en) * 1996-10-11 1999-09-14 Gary D. Fields Apparatus to make building blocks for blockwork domed structures, and method and domed structure
JPH10156853A (en) 1996-11-29 1998-06-16 Meiki Co Ltd Vacuum multiple laminating machine
JPH10244589A (en) 1997-03-06 1998-09-14 Fuji Electric Co Ltd Laminating device
US20030089214A1 (en) * 1998-11-05 2003-05-15 Ngk Insulators, Ltd. Cutting apparatus for ceramic green bodies
JP2000141388A (en) 1998-11-06 2000-05-23 Nichigo Morton Co Ltd Method for laminating
US6832538B1 (en) * 2000-01-06 2004-12-21 Ber-Fong Hwang Foam sponge cutting apparatus with both vertical and horizontal cutting devices
US6388724B1 (en) 2000-05-02 2002-05-14 Rockwell Collins, Inc. Apparatus having a platen with pins and standoffs, used to laminate an LCD to other optical components using silicone gel
US6681668B1 (en) * 2000-08-25 2004-01-27 Steven John Smirle Device and process for thermally cutting a moving web of textile material
US6614057B2 (en) 2001-02-07 2003-09-02 Universal Display Corporation Sealed organic optoelectronic structures
US6803245B2 (en) 2001-09-28 2004-10-12 Osram Opto Semiconductors Gmbh Procedure for encapsulation of electronic devices
US7273403B2 (en) 2001-12-27 2007-09-25 Kabushiki Kaisha Toshiba Method of manufacturing flat display panels of different sizes from a common base substrate
US20030180528A1 (en) 2002-03-22 2003-09-25 Eastman Kodak Company Cellulose film with anti-blocking properties
US6984545B2 (en) 2002-07-22 2006-01-10 Micron Technology, Inc. Methods of encapsulating selected locations of a semiconductor die assembly using a thick solder mask
JP2004233590A (en) 2003-01-29 2004-08-19 Kyocera Corp Pressing device
US6998648B2 (en) 2003-08-25 2006-02-14 Universal Display Corporation Protected organic electronic device structures incorporating pressure sensitive adhesive and desiccant
US20050126679A1 (en) 2003-12-13 2005-06-16 Kwang-Jin Kim Apparatus and method for fabricating liquid crystal display
JP2006218658A (en) 2005-02-08 2006-08-24 Fuji Electric Holdings Co Ltd Vacuum laminator and vacuum lamination method
US20060245171A1 (en) 2005-04-29 2006-11-02 Sok-San Kim Plasma display module
JP2006334912A (en) 2005-06-01 2006-12-14 Dainippon Printing Co Ltd Lamination device
US20090120585A1 (en) 2005-08-30 2009-05-14 Sampica James D Substrate lamination system and method
US20090126872A1 (en) 2005-08-30 2009-05-21 Sampica James D System and method for completing lamination of rigid-to-rigid substrates by the controlled application of pressure
US7381110B1 (en) 2005-08-30 2008-06-03 Rockwell Collins, Inc. Process for applying a protective cover on an organic light-emitting diode using a liquid adhesive
US20090120572A1 (en) 2005-08-30 2009-05-14 Sampica James D Substrate lamination system and method
US7435311B1 (en) 2005-08-30 2008-10-14 Rockwell Collins, Inc. Panel-to-panel lamination method for improved uniformity
US7452258B1 (en) 2005-08-30 2008-11-18 Rockwell Collins, Inc. Method of sealing OLED cover with liquid adhesive
JP2007206559A (en) 2006-02-03 2007-08-16 Yamaichi Electronics Co Ltd Method for removing film for liquid crystal display panel
US20070297736A1 (en) 2006-06-27 2007-12-27 3M Innovative Properties Company Rigid optical laminates and methods of forming the same
JP2008238607A (en) 2007-03-28 2008-10-09 Tafu:Kk Thin-film type laminating apparatus and lamination method using the same
US20090183381A1 (en) 2008-01-18 2009-07-23 Sampica James D Alignment system and method thereof
US20090186218A1 (en) 2008-01-18 2009-07-23 Sampica James D Planarization treatment of pressure sensitive adhesive for rigid-to-rigid substrate lamination
US7814676B2 (en) 2008-01-18 2010-10-19 Rockwell Collins, Inc. Alignment system and method thereof

Non-Patent Citations (10)

* Cited by examiner, † Cited by third party
Title
Notice of Allowance for U.S. Appl. No. 12/009,373, mail date Jun. 16, 2010, 4 pages.
Office Action for U.S. Appl. No. 12/009,472, mail date Jan. 14, 2011, 14 pages.
U.S. Appl. No. 11/214,518, filed Aug. 30, 2005, Sampica et al.
U.S. Appl. No. 12/009,373, filed Jan. 18, 2008, Sampica et al.
U.S. Appl. No. 12/009,375, filed Jan. 18, 2008, Sampica et al.
U.S. Appl. No. 12/009,393, filed Jan. 18, 2008, Barnidge et al.
U.S. Appl. No. 12/009,472, filed Jan. 18, 2008, Sampica et al.
U.S. Appl. No. 12/009,482, filed Jan. 18, 2008, Sampica et al.
US Office Action for U.S. Appl. No. 12/009,373 , mail date Dec. 30, 2009, 14 pages.
Walker, Geoff, GD-Itronix Dynavue Technology, The Ultimate Outdoor-Readable Touch-Screen Display, Rugged PC Review, pp. 1-4, United States of America.

Cited By (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8746311B1 (en) 2005-08-30 2014-06-10 Rockwell Collins, Inc. System and method for completing lamination of rigid-to-rigid substrate by the controlled application of pressure
US20090120585A1 (en) * 2005-08-30 2009-05-14 Sampica James D Substrate lamination system and method
US8936057B2 (en) 2005-08-30 2015-01-20 Rockwell Collins, Inc. Substrate lamination system and method
US8540002B2 (en) 2005-08-30 2013-09-24 Rockwell Collins, Inc. System and method for completing lamination of rigid-to-rigid substrates by the controlled application of pressure
US9733349B1 (en) 2007-09-06 2017-08-15 Rockwell Collins, Inc. System for and method of radar data processing for low visibility landing applications
US9939526B2 (en) 2007-09-06 2018-04-10 Rockwell Collins, Inc. Display system and method using weather radar sensing
US20090186218A1 (en) * 2008-01-18 2009-07-23 Sampica James D Planarization treatment of pressure sensitive adhesive for rigid-to-rigid substrate lamination
US9638944B1 (en) 2008-01-18 2017-05-02 Rockwell Collins, Inc. Systems and methods for substrate lamination
US9573327B2 (en) 2008-01-18 2017-02-21 Rockwell Collins, Inc. Planarization treatment of pressure sensitive adhesive for rigid-to-rigid substrate lamination
US8603288B2 (en) 2008-01-18 2013-12-10 Rockwell Collins, Inc. Planarization treatment of pressure sensitive adhesive for rigid-to-rigid substrate lamination
US8419896B2 (en) * 2008-11-20 2013-04-16 E. I. Du Pont De Nemours And Company Semi-automated reworkability process for de-bonding a display
US20110180218A1 (en) * 2008-11-20 2011-07-28 E.I. Du Pont De Nemours And Company Semi-automated reworkability process for de-bonding a display
US9409383B2 (en) * 2008-12-22 2016-08-09 Apple Inc. Layer-specific energy distribution delamination
US20100154992A1 (en) * 2008-12-22 2010-06-24 Feinstein Casey J Layer-Specific Energy Distribution Delamination
US20120263956A1 (en) * 2009-10-16 2012-10-18 Sony Chemical & Information Device Corporation Display, manufacturing method therefor and transparent resin charging material
US9182625B2 (en) * 2009-10-16 2015-11-10 Dexerials Corporation Display, manufacturing method therefor and transparent resin charging material
US8486535B1 (en) 2010-05-24 2013-07-16 Rockwell Collins, Inc. Systems and methods for adherable and removable thin flexible glass
US8261804B1 (en) * 2011-10-28 2012-09-11 Meicer Semiconductor Inc. IC layers separator
US8647727B1 (en) 2012-06-29 2014-02-11 Rockwell Colllins, Inc. Optical assembly with adhesive layers configured for diffusion
US11097439B2 (en) 2012-10-17 2021-08-24 Saxum, Llc Method and apparatus for display screen shield replacement
US10220537B2 (en) 2012-10-17 2019-03-05 Saxum, Llc Method and apparatus for display screen shield replacement
US8956501B2 (en) 2012-10-17 2015-02-17 Saxum LLC Method and apparatus for display screen shield replacement
US8888953B2 (en) 2012-10-17 2014-11-18 Saxum LLC Method and apparatus for display screen shield replacement
US8960255B2 (en) * 2012-11-09 2015-02-24 Boe Technology Group Co., Ltd. Film stripping mechanism
US20140130987A1 (en) * 2012-11-09 2014-05-15 Boe (Hebei) Mobile Display Technology Co., Ltd. Film stripping mechanism
US9384586B1 (en) 2013-04-05 2016-07-05 Rockwell Collins, Inc. Enhanced flight vision system and method with radar sensing and pilot monitoring display
US20140338828A1 (en) * 2013-05-14 2014-11-20 Samsung Display Co., Ltd. Substrate separation apparatus and method
US9125295B2 (en) * 2013-05-14 2015-09-01 Samsung Display Co., Ltd. Substrate separation apparatus and method
US9254636B2 (en) 2013-09-24 2016-02-09 Apple Inc. Display module reworkability
US20150197024A1 (en) * 2014-01-15 2015-07-16 Southwest Research Institute Method And Apparatus To Propagate Crack Growth In A Workpiece
US9573284B2 (en) * 2014-01-15 2017-02-21 Southwest Research Institute Method and apparatus to propagate crack growth in a workpiece
US9981460B1 (en) 2014-05-06 2018-05-29 Rockwell Collins, Inc. Systems and methods for substrate lamination
US10928510B1 (en) 2014-09-10 2021-02-23 Rockwell Collins, Inc. System for and method of image processing for low visibility landing applications
US20160195968A1 (en) * 2015-01-06 2016-07-07 Boe Technology Group Co., Ltd. Method and system for separating touch panel from display module
US10052777B2 (en) * 2015-01-06 2018-08-21 Boe Technology Group Co., Ltd. Method and system for separating touch panel from display module
US9862115B2 (en) * 2015-03-27 2018-01-09 Intel Corporation Hidden feature for accessing or repairing mobile devices
US10618192B2 (en) 2015-03-27 2020-04-14 Intel Corporation Hidden feature for accessing or repairing mobile devices
US20160279862A1 (en) * 2015-03-27 2016-09-29 Intel Corporation Hidden feature for accessing or repairing mobile devices
US20160375600A1 (en) * 2015-06-29 2016-12-29 Igor Markovsky Joint cutting in a device
US10705201B1 (en) 2015-08-31 2020-07-07 Rockwell Collins, Inc. Radar beam sharpening system and method
US20180354251A1 (en) * 2015-10-30 2018-12-13 Corning Incorporated Methods for processing a first substrate bonded to a second substrate
US10814603B2 (en) * 2015-10-30 2020-10-27 Corning Incorporated Methods for processing a first substrate bonded to a second substrate
US11548084B2 (en) * 2016-03-15 2023-01-10 Saint-Gobain Placo Method and device for cutting a plate or panel of porous construction material
US10228460B1 (en) 2016-05-26 2019-03-12 Rockwell Collins, Inc. Weather radar enabled low visibility operation system and method
US10955548B1 (en) 2016-05-26 2021-03-23 Rockwell Collins, Inc. Weather radar enabled low visibility operation system and method
US10353068B1 (en) 2016-07-28 2019-07-16 Rockwell Collins, Inc. Weather radar enabled offshore operation system and method

Also Published As

Publication number Publication date
US20090183615A1 (en) 2009-07-23

Similar Documents

Publication Publication Date Title
US8118075B2 (en) System and method for disassembling laminated substrates
US9126393B2 (en) Bonding apparatus and method of bonding component on substrate using the same
US20090183381A1 (en) Alignment system and method thereof
TW201113600A (en) Method and system for continuously manufacturing liquid-crystal display element
US10315406B2 (en) Film-like structure, film removing device and film removing method
WO2007069421A1 (en) Adhesive tape-joining device and adhesive tape-adhering device
KR102522358B1 (en) Manufacturing method of display device and apparatus for manufacturing display device
JP5996241B2 (en) Adhesive film sticking device, adhesive film sticking method, and connection structure
JP2007047304A (en) Manufacturing apparatus and method of liquid crystal display apparatus, and liquid crystal display apparatus
TW200848346A (en) Apparatus for cutting an adhesive film, equipment for sticking an adhesive film having the same, method for cutting an adhesive film using the same, and method for sticking an adhesive film using the same
JP2016038436A (en) Display panel, and device and method of peeling cover glass
JP2009073645A (en) Adhesive tape sticking device and method of detecting residual amount of tape
TW201243430A (en) Automatic processing system for liquid crystal panel
JP2012218353A (en) Elongate material with pattern structure layer and method of pasting the pattern structure layer
TW201535180A (en) Touch panel and method of attaching same
WO2013177818A1 (en) Vacuum laminating machine and operating method thereof
CN114852448B (en) Protective film peeling device and peeling method using same
JP2009186497A (en) Apparatus for manufacturing liquid crystal display panel and method of manufacturing liquid crystal display panel
JP4417893B2 (en) Adhesive tape sticking device and sticking method
JP2011142139A (en) Acf sticking device
KR100669792B1 (en) Method of manufacturing a forming substrate, method of manufacturing a flat panel display device thereused, and pre-bonding apparatus of flexible substrate
KR100659117B1 (en) Align recognition apparatus of flexible substrate
JP4778404B2 (en) Sticking device
TWI468787B (en) Temporary bonding method and bonding apparatus thereof
US5393359A (en) Method and apparatus for bonding outer leads of a liquid crystal display to metal leads of a bonding tape

Legal Events

Date Code Title Description
AS Assignment

Owner name: ROCKWELL COLLINS, INC., IOWA

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:SAMPICA, JAMES D.;NEMETH, PAUL R.;BARNIDGE, TRACY J.;AND OTHERS;REEL/FRAME:020446/0391

Effective date: 20080118

FEPP Fee payment procedure

Free format text: PAYOR NUMBER ASSIGNED (ORIGINAL EVENT CODE: ASPN); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

STCF Information on status: patent grant

Free format text: PATENTED CASE

FPAY Fee payment

Year of fee payment: 4

MAFP Maintenance fee payment

Free format text: PAYMENT OF MAINTENANCE FEE, 8TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1552); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

Year of fee payment: 8

MAFP Maintenance fee payment

Free format text: PAYMENT OF MAINTENANCE FEE, 12TH YEAR, LARGE ENTITY (ORIGINAL EVENT CODE: M1553); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY

Year of fee payment: 12